论文

EXPERIMENTAL RESEARCH AND NUMERICAL SIMULATION OF SOLIDIFICATION CRACK DURING LASER WELDING OF RING STRUCTURE

  • YUN Peng
Expand
  • 1.Mechanical Engineering Department, Tsinghua University, Beijing 10084
    2.Department of Mechanical Engineering, Hiroshima University, Hiroshima 739–8527, Japan

Received date: 2011-03-29

  Revised date: 2011-05-06

  Online published: 2011-10-11

Abstract

The combined influence of metallurgical and mechanical factors on welding solidification cracking structure in laser welded ring was investigated by using both experiments and numerical simulation. It is found that solidification cracking is directly related with the overlap weld part. The microstructure was observed under OM, and the grain size was measured by EBSD observation. The grains in overlap weld part are much bigger than those in single weld part, which results in falling of ductility during solidification. The temperature and strain changes of weld metal in solidification temperature range were calculated out by using 3D finite element analysis. Compared with the single weld part, the strain rate with temperature drop is lower in overlap weld part, i.e., the mechanical driving force to solidification cracking is weaker in overlap weld part. Consequently, it is concluded that the low ductility caused by coarse grain results in the occurrence of solidification cracking in overlap weld part during laser welding of ring structure. This research not only helps to understand the mechanism of solidification cracking in more details, but also guides the study on prediction of solidification cracking occurrence.

Cite this article

YUN Peng . EXPERIMENTAL RESEARCH AND NUMERICAL SIMULATION OF SOLIDIFICATION CRACK DURING LASER WELDING OF RING STRUCTURE[J]. Acta Metall Sin, 2011 , 47(10) : 1241 -1245 . DOI: 10.3724/SP.J.1037.2011.00174

References

[1] Fang H Y, Wang X T, Fang C L, Yang J G. Trans China Weld Inst, 2004; 25(4): 73

(方洪渊, 王霄腾, 范成磊, 杨建国. 焊接学报, 2004; 25(4): 73)

[2] Kou S. Welding Metallurgy. 2nd Ed., New Jersey: John Wiley & Sons, 2002: 263

[3] Li X H, Mao W, Xiong H P. J Aeronaut Mater, 2006; 26: 276

(李晓红, 毛唯, 熊华平. 航空材料学报, 2006; 26: 214)

[4] Kim Y C, Garatani K. Weld J, 1993; 72: 51

[5] Chen X Z, Shen Z, Li D S. J Shanghai Jiaotong Univ, 2010; 44: 29

(陈希章, 沈政, 李冬升. 上海交通大学学报, 2010; 44: 29)

[6] Dong Z B, Wei Y H, Liu R P, Dong Z J. Acta Metall Sin, 2005; 41: 214

(董志波, 魏艳红, 刘仁培, 董祖珏. 金属学报, 2005; 41: 214)

[7] Wen P, Shinozaki K, Yamamoto M, Tamura T, Nemoto N. Q J Jpn Weld Soc, 2009; 27: 139

[8] Feng Z L. PhD Thesis, Ohio State University, 1993

[9] Nakata K, Matsuda F. Q J Jpn Weld Soc, 1995; 13: 106

[10] Houldcroft P T. Br Weld J, 1955; 2: 471

[11] Shinozaki K. Q J Jpn Weld Soc, 2002; 71: 43

[12] Savage W F, Lundin C D. Weld J, 1965; 44: 433s

[13] Dupont J N, Michael J R, Newbury B D. Weld J, 1999; 78: 408s

[14] Matsuda F, Nakagawa H, Tomita S. Q J Jpn Weld Soc, 1988; 6: 394

[15] Wei Y H, Liu R P, Dong Z J. Sci Technol Weld Joining, 2003; 8: 325
Outlines

/